[fltsim.0]
title=P540
sim=P540
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=540
ui_manufacturer=Potez
ui_type="540"
ui_variation="French Green"
description="The Potez 540 was a French multi-role aircraft of the 1930s. Designed and built by Potez, it served with the French Air Force as a Reconnaissance Bomber, also serving with the Republican side during the Spanish Civil War. Although obsolete as a bomber, it remained in service in support roles and in France's overseas colonies at the start of the Second World War."
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
[General]
atc_type=Potez
atc_model=540
editable=0
performance="Cruise speed\n160 mph\n\nEngines\nTwo Hispano_Suiza V-12's rated at 700 hp\n\nMaximum range\n777 miles\n\nService ceiling\n32810 feet\n\nEmpty weight\n8344 lb\n\nMaximum gross weight\n13115 lb\n\nLength\n53' 2"\n\nWingspan\72' 6"\n\n\n Designer: P. Clawson 9/2008\\n"
Category=airplane
[weight_and_balance]
// ACM V2.5
max_gross_weight = 13115
empty_weight = 8344
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 69699.03
empty_weight_roll_MOI = 61179.1
empty_weight_yaw_MOI = 131797.97
empty_weight_coupled_MOI = 0
max_number_of_stations = 12
station_load.0 = "170.0, -5.4, -2.0, 0.0, Pilot"
station_load.1 = "170.0, -5.4, 2.0, 0.0, Co-Pilot"
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 4, 3.46, 0.0, 3.1, fx_vclight,
light.1 = 3, 2.972, -28.21, 3.95, fx_navredm ,
light.2 = 3, 2.972, 28.21, 3.95, fx_navgrem ,
//light.3 = 3, -38.52, 0.00, 2.502, fx_navwhi ,
//light.4 = 5, 2.41, 20.828, 3.86, fx_landing ,
//light.5 = 5, 2.41, -20.828, 3.86,fx_landing ,
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 1.0
min_throttle_limit = 0.0
master_ignition_switch = 1
engine.0 = 4.25, -8.07, -1.24,
engine.1 = 4.25, 8.07, -1.24,
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
startup = fx_engstrt_jenny
windshield_rain_effect_available = 1
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1
number_of_tank_selectors = 2
electric_pump = 1
Center1 = 0, -0.01, -2.70, 200, 0
LeftMain = 0.16, -8.06, -3, 202, 0
RightMain = -0.24, 7.91, -3, 202, 0
[contact_points]
static_pitch = 10.8
static_cg_height = 7.75
tailwheel_lock = 1
gear_system_type = 1
max_number_of_points = 7
point.0 = 1, -36.3018, 0, -1.45, 1200, 0, 0.75, 22, 0.2, 2.5, 0.695, 0, 0, 0, 0, 0
point.1 = 1, 1.0547, -8.3289, -8.45, 1600, 1, 1.75, 0, 0.54, 2.5, 0.65, 5, 5, 7, 166, 166
point.2 = 1, 1.1443, 7.9601, -8.45, 1600, 2, 1.75, 0, 0.54, 2.5, 0.65, 6, 5, 7, 166, 166
point.3 = 2, -1.7066, -34.5135, 2.6884, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.7175, 34.4253, 2.8157, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -38.1199, 0, 0.5358, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 13.393, 0, -3.8291, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
[keyboard_response]
elevator = 200, 1000
aileron = 200, 1000
rudder = 200, 1000
[forcefeedback]
ground_bumps_magnitude1 = 2600
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.6
ground_bumps_magnitude2 = 1200
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.085
ground_bumps_slope2 = 0.65
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 3500000
[airplane_geometry]
wing_area = 987.0
wing_span = 72.73
wing_root_chord = 12.47
wing_dihedral = 1
wing_incidence = 2.0
wing_twist = -1.0
oswald_efficiency_factor = 0.65
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2.66
wing_pos_apex_vert = 3.91
htail_area = 95.8
htail_span = 23.45
htail_pos_lon = -30.38
htail_pos_vert = 2.55
htail_incidence = -1.0
htail_sweep = 8
vtail_area = 37.9
vtail_span = 8.81
vtail_sweep = 35
vtail_pos_lon = -28.73
vtail_pos_vert = 2.64
elevator_area = 83.4
aileron_area = 102.8
rudder_area = 46.7
elevator_up_limit = 30.0
elevator_down_limit = 20.0
aileron_up_limit = 27.0
aileron_down_limit = 18.0
rudder_limit = 30.0
elevator_trim_limit = 12.0
spoiler_limit = 0.0
aileron_to_spoileron_gain = 0
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0
auto_spoiler_available=0
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-1.500000
negative_g_limit_flaps_down=-1.500000
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 25
max_generator_alternator_amps = 100
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
p_factor_on_yaw = 0.5
torque_on_roll = 1.0
gyro_precession_on_yaw = 1.0
gyro_precession_on_pitch = 1.0
[piston_engine]
power_scalar=1.0 //Piston power scalar
cylinder_displacement=183 //Cubic inches per cylinder
compression_ratio=6.7 //Compression ratio
number_of_cylinders=12 //Number of cylinders
max_rated_rpm=2700 //Max rated RPM
max_rated_hp=700 //Max rated HP
fuel_metering_type=1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type=0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.3 //Starter torque factor
turbocharged=1 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=47 //Max design manifold pressure, (inHg)
min_design_mp=10 //Min design manifold pressure, (inHg)
critical_altitude=7000 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type=0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset=0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset=0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture=0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition=0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar=1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar=1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar=1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar=1.0 //Scalar on idle RPM friction
[propeller]
thrust_scalar=1.0 //Propeller thrust scalar
propeller_type=0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=11.53 //Propeller Diameter, (feet)
propeller_blades=3 //Number of propeller blades
propeller_moi=40.2 //Propeller moment of inertia
beta_max=30.0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=18.0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=1400 //Miminum governed RPM
prop_tc=0.1 //Prop time-constant
gear_reduction_ratio=1.778 //Propeller gear reduction ratio
fixed_pitch_beta=0.0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80.0 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=1 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available=0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather=700.0 //Minimum RPM for prop feathering
beta_feather=89.5 //Feathering pitch angle (degrees)
power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propeller in feather
defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta=0.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=0.0 //Minimum pitch angle in reverse, (degrees)
feathering_switches=1 //Switches which invoke feathering
//0 Class
//1 Longitudinal Position (feet)
//2 Lateral Position (feet)
//3 Vertical Position (feet)
//4 Impact Damage Threshold (Feet Per Minute)
//5 Brake Map (0=None, 1=Left, 2=Right)
//6 Wheel Radius (feet)
//7 Steer Angle (degrees)
//8 Static Compression (feet) (0 if rigid)
//9 Max/Static Compression Ratio
//10 Damping Ratio (0=Undamped, 1=Critically Damped)
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 0.0 //Flap angle that activates warning at idle
flap_limit_power = 16.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.9 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
[hydraulic_system]
normal_pressure = 732.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[Views]
eyepoint=3.3, -1.0, 3.1
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Adf.2 = 1
Transponder.1=0
Marker.1=1
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=1,0
direction_indicator.1=2,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
attitude_indicator.1 = 2
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=2,0
[Reference Speeds]
flaps_up_stall_speed=67.5 //Knots True (KTAS)
full_flaps_stall_speed=61.5 //Knots True (KTAS)
cruise_speed=95.0 //Knots True (KTAS)
max_indicated_speed = 224 //Red line (KIAS)
[autopilot]
autopilot_available=0
flight_director_available=0
pitch_takeoff_ga=0.0
default_vertical_speed=700.000000
autothrottle_available=0
direction_indicator=1
attitude_indicator =1
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain = 0.0
default_bank_mode=2 //Default to Heading Hold
[stall_warning]
type=1
stick_shaker=0
[exits]
number_of_exits = 1
exit_rate.0 = 0.4 ;Percent per second
[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,1,0,0
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0
[Flaps.0]
type=0
span-outboard=0.500000
extending-time=0.000000
system_type=0
